Chemical and Radiative Size—Related Effects on the Performance of Liquid Rocket Engines fed with Different Propellant Combinations
Crossref DOI link: https://doi.org/10.1007/BF03404690
Published Online: 2015-04-01
Published Print: 2015-04
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Lentini, D.
Text and Data Mining valid from 2015-04-01